摘要: A multi-input, multi-output controls design with robust crossfeeds is presentedfor a rotorcraft in near-hovering flight using quantitative feedback theory (QFT). Decoupling criteria are developed for dynamic crossfeed design and i... 展开
作者 | Cheng, R. P. | ||
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原报告号 | N9621276 | 总页数 | 87 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Control systems design Cross coupling Feedback control Flight control Helicopter control Hovering Mimo (Control systems) Rotary wing aircraft Compensators Control theory Controllability Decoupling Manual control |